ISO 17770:2017 PDF
Space systems — Cube satellites (CubeSats)
Space systems — Cube satellites (CubeSats)
- Статус документа:
- Действующий
- Формат:
- Электронный (PDF)
- Количество страниц:
- 9
- Дата публикации:
- 26 июня 2017 г.
- Издание:
- ISO IS 17770 edition 1 version 1
- ICS:
- 49.140
ISO 17770:2017 addresses CubeSats, CubeSat Deployer and related verification of assurance/quality terms and metrics. ISO 17770:2017 defines a unique class of picosatellite, the CubeSat. CubeSats are ideal as space development projects for universities around the world. In addition to their significant role in educating space scientists and engineers, CubeSats provide a low-cost platform for testing and space qualification of the next generation of small payloads in space. A key component of the project is the development of a standard CubeSat Deployer. This Deployer is capable of releasing a number of CubeSats as secondary payloads on a wide range of launchers. The standard Deployer requires all CubeSats to conform to common physical requirements, and share a standard Deployer interface. CubeSat development time and cost can be significantly reduced by the development of standards that are shared by a large number of spacecraft. Normative control of the CubeSat design, qualification and acceptance testing is generally applied from other small satellite specific standards with the exception of CubeSat/Deployer launch environment test.
Abstract
Overview
ISO 17770:2017 - Space systems - Cube satellites (CubeSats) defines the physical form factor, interface and basic verification/assurance criteria for CubeSats and the standard CubeSat Deployer. The standard formalizes the picosatellite class (commonly 1U and 3U CubeSats), enabling low-cost, repeatable small-satellite development, standardized launch integration and predictable deployment as secondary payloads on a wide range of launch vehicles.
Key Topics and Requirements
- Form factor and units: 1U CubeSat = 100 mm × 100 mm × 113.5 mm (±0.1 mm); 3U (triple) = 340.5 mm (±0.3 mm). Components may not protrude more than 6.5 mm from cube faces.
- Mass limits: 1U ≤ 1.33 kg; 3U ≤ 4.00 kg.
- Interface rails: rail minimum width 8.5 mm, surface roughness
Технические детали
- Технический комитет
- ISO/TC 20/SC 14 - Space systems and operations
- SKU
- ISO 17770:2017
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